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- W3148689215 abstract "当飞机震动撞击楔时，出发在上，它经历一个思考衍射过程然后自我类似的反映的震动作为吃惊及时向前移动的原版向外移动。在这份报纸，由为非线性的波浪方程建模的可压缩的流动的大角度的楔的吃惊思考被学习，存在，稳定性和整齐的一个全球理论被建立。而且， C 0,1 是为越过退化声音的边界的答案的最佳的整齐。" @default.
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- W3148689215 date "2011-01-01" @default.
- W3148689215 modified "2023-09-24" @default.
- W3148689215 title "Global Solutions of Shock Reflection by Wedges for the Nonlinear Wave Equation" @default.
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